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DPW-W1, W2
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DPW-W1, W2. Geometry. b = wing span = 1524. mm S ref = reference area = 290.322 mm 2 AR = aspect ratio = b 2 / S ref = 8.0 L.E. sweep angle = 17.2 degrees T.E. sweep angle = 15.0 degrees. Wing Flow Conditions. M = inlet Mach number = 0.76 Compressible flow
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DPW-W1, W2
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Geometry • b = wing span = 1524. mm • Sref= reference area = 290.322 mm2 • AR = aspect ratio = b2/Sref = 8.0 • L.E. sweep angle = 17.2 degrees • T.E. sweep angle = 15.0 degrees
Wing Flow Conditions • M = inlet Mach number = 0.76 • Compressible flow • ReL = Reynolds number = 5,000,000 • Turbulent flow • = angle of attack = -1.0, 0.0, 0.5, 1.0, 1.5, 2.0, 2.5, 3.0
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